The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 27, 2020

Filed:

Jan. 20, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Richard Martin DiCintio, Simpsonville, SC (US);

Seth Reynolds Hoffman, Spartanburg, SC (US);

Jayaprakash Natarajan, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/28 (2006.01); F02C 3/04 (2006.01); F01D 9/04 (2006.01); F23R 3/34 (2006.01);
U.S. Cl.
CPC ...
F23R 3/286 (2013.01); F01D 9/041 (2013.01); F02C 3/04 (2013.01); F23R 3/283 (2013.01); F23R 3/346 (2013.01); F05D 2220/32 (2013.01); F05D 2230/50 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01);
Abstract

A fuel injector for a gas turbine combustor includes a fuel conduit fitting and a nozzle having an inlet portion defining a mixing chamber therein. The inlet portion includes a plurality of circumferentially-spaced vanes that define a plurality of inlet flow paths within the mixing chamber. Each vane has at least one port defined therein that is in flow communication with the fuel conduit fitting such that fuel from the fuel conduit fitting is dischargeable into at least one of the inlet flow paths via the at least one port. The resulting fuel/air mixture is delivered into a secondary combustion zone of the gas turbine combustor. A gas turbine including the fuel injector and a method of fabricating the fuel nozzle are also provided.


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